US8136574B2 - Multi-piece piston for a cold chamber casting machine - Google Patents
Multi-piece piston for a cold chamber casting machine Download PDFInfo
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- US8136574B2 US8136574B2 US11/992,716 US99271606A US8136574B2 US 8136574 B2 US8136574 B2 US 8136574B2 US 99271606 A US99271606 A US 99271606A US 8136574 B2 US8136574 B2 US 8136574B2
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- United States
- Prior art keywords
- piston
- pressure side
- cover
- end region
- piston rod
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D17/00—Pressure die casting or injection die casting, i.e. casting in which the metal is forced into a mould under high pressure
- B22D17/20—Accessories: Details
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D17/00—Pressure die casting or injection die casting, i.e. casting in which the metal is forced into a mould under high pressure
- B22D17/20—Accessories: Details
- B22D17/2015—Means for forcing the molten metal into the die
- B22D17/203—Injection pistons
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D17/00—Pressure die casting or injection die casting, i.e. casting in which the metal is forced into a mould under high pressure
- B22D17/08—Cold chamber machines, i.e. with unheated press chamber into which molten metal is ladled
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D17/00—Pressure die casting or injection die casting, i.e. casting in which the metal is forced into a mould under high pressure
- B22D17/20—Accessories: Details
- B22D17/2015—Means for forcing the molten metal into the die
- B22D17/2038—Heating, cooling or lubricating the injection unit
Definitions
- the invention relates to a multi-piece piston to be fastened to the high-pressure side end region of a piston rod displaceable axially in a casting cylinder of a cold chamber casting machine.
- the conventionally cooled pistons of cold chamber casting machines are subject to relatively high wear during operation. Exchanging the piston or the wearing parts of the piston is detrimental to the productivity of the casting machine.
- the exchange of worn pistons takes a comparatively long time and special tools are often required, particularly since components of the piston and of the piston rod become jammed or clogged up during operation and can often only be released by force.
- a piston cover forming a piston end wall on the high-pressure side is to be screw-connected to a piston body, adjoining the piston cover on the low-pressure side, in the form of a bush surrounding the piston carrier of the piston rod.
- the configuration makes it possible to produce the piston cover from a material other than that of the piston body, in order to implement different heat conduction conditions on the piston end wall, on the one hand, and the piston body, on the other hand.
- the divisibility of the piston makes it easier to change wearing rings of the piston, in so far as these overlap axially with the parting plane of the piston. It has been shown, however, that the screw connection between the piston cover and the piston body tends to experience wear during casting operation and that jamming and clogging cannot be ruled out.
- the object of the invention is to provide a multi-piece piston for a cold chamber casting machine, which, in the event of wear, can easily be exchanged as a whole or at least in pieces.
- the invention proceeds from a multi-piece piston to be fastened to the high-pressure side end region of a piston rod displaceable axially in a casting cylinder of a cold chamber casting machine and comprises:
- the fastening members comprise bayonet locking members axially fixing the piston cover in itself to the end region of the piston rod.
- Such a bayonet connection transmits tensile forces acting on the piston cover when the piston rod is being drawn back out of the casting cylinder directly to the end region of the piston rod. This reduces the risk of problems arising during the exchange of wearing parts.
- the design and production of the piston are simplified.
- the bush forming the piston body can be produced more simply than in conventional multi-piece pistons.
- pistons with a large piston diameter Since the end region of the piston carrier usually consists of a tough material, vibration problems may occur during the milling of the piston-rod side bayonet locking member, if these are arranged at a comparatively long distance from the end face, as is usually customary. Conventional pistons with a large diameter have therefore had to possess a comparatively short axial dimensioning in relation to the diameter, which may lead to sealing problems and cooling problems.
- the piston according to the invention can be produced even for relatively large piston diameters with a ratio of axial length to piston diameter of between 0.8 and 1, as has proved beneficial for pistons with a comparatively small diameter.
- the bayonet locking members to fix the piston cover to the end region of the piston rod with axial play, in such a way that the piston end wall can be brought into axial bearing contact with the axial end face of the end region of the piston rod and can be lifted off axially from the latter. Consequently, during operation, the piston end wall can be supported over a large area on the end region of the piston rod and can discharge the pressure forces occurring during casting into the piston rod over a large area.
- the piston end wall can therefore have a comparatively thin dimensioning, thus making it easier to cool the piston.
- the piston can nevertheless be demounted without difficulty.
- the bayonet locking members are expediently arranged near the axial end face of the end region of the piston rod, for example in such a way that the bayonet locking members have a plurality of pairs of mutually assigned locking projections on the piston cover and on the end region of the piston rod, at least the locking projections provided on the end region of the piston rod being arranged axially in front of the piston body toward the high-pressure side.
- the locking projections assigned to the piston cover may, if appropriate, overlap axially with the piston body and be utilized for the radial centering of the piston body on the piston cover.
- the piston is expediently cooled by a cooling fluid which is supplied and discharged via connecting ducts of the piston rod and of its end region.
- a cooling fluid which is supplied and discharged via connecting ducts of the piston rod and of its end region.
- coolant ducts are formed which are connected to one another via interspaces located in the circumferential direction between bayonet locking members.
- the connecting ducts expediently issue in the center of the end face of the end region of the piston rod and in the region of the low-pressure side end of the piston body. It is thereby possible, contrary to conventional pistons, to bring essentially the entire piston into contact with the coolant.
- the end region of the piston rod has, in the region of the axial overlap by the piston body, groove regions which are separated from one another by supporting webs and which form the coolant ducts.
- the piston body can be supported radially on the supporting webs.
- the groove regions expediently extend essentially in the circumferential direction of the end region of the piston rod.
- the groove regions may run in axially normal planes or else be designed as single-flight or multi-flight helical grooves.
- the bush forming the piston body may be connected to the piston cover via fastening members to form a structural unit, but may also be fixed axially in itself solely between abutment surfaces.
- at least one abutment element for fixing the piston body in the axial direction and/or in the circumferential direction may be provided in the end region of the piston rod, said abutment element preferably being fastened removably to the end region of the piston rod, for example being screwed thereto by means of a screw running radially with respect to the end region.
- the abutment element engages into a clearance, delimited on both sides in a circumferential direction, at the low-pressure side axial end of the piston body and thus at the same time ensures an anti-twist device for the piston body in relation to the piston rod.
- a plurality of such abutment elements are preferably provided, distributed in the circumferential direction.
- the abutment element in a preferred refinement which also has independent inventive significance, that is to say may also be used in pistons other than those explained above, in particular also in one-piece pistons, there is provision for the abutment element to have an abutment surface which is obliquely inclined radially outward with respect to the piston end wall and which bears against a codirectionally inclined countersurface of the piston body. Setting the abutment surfaces obliquely reduces the risk of clogging and makes it easier to demount used pistons.
- the multi-piece nature of the piston makes it possible to produce the piston cover and the piston body from different materials, so that the individual components of the piston can thereby be adapted better to their respective functional purpose. Furthermore, the multi-piece nature of the piston makes it possible to design exchangeable wearing parts which are lighter than hitherto.
- the piston cover may carry on its outer circumferential surface, in an annular clearance open toward the low-pressure side, a slotted radially resilient wearing ring which is fixed axially by a snap ring fixed axially on its low-pressure side to the piston cover.
- the snap ring may also be utilized for fixing a wearing ring or such a bush surrounding the piston body, even when both wearing rings are slotted and come radially to bear resiliently against the casting cylinder.
- a closed wearing ring may also be shrunk with a press fit on the outer circumferential surface of the piston cover. Even such a wearing ring can be changed if it is cut open axially for this purpose. It will be appreciated that even a plurality of wearing rings may be shrunk on axially next to one another, so that even wearing rings consisting of different materials can be used closely next to one another.
- the outer circumferential surface of the piston cover and/or of the piston body may be adapted as such to the inside diameter of the casting cylinder, so that the piston cover and the piston body serve themselves as wearing parts.
- the piston cover may carry on its outer circumferential surface, in an annular clearance open toward the high-pressure side, a slotted wearing ring which, in the region of its low-pressure side axial end, has a radially inwardly projecting annular projection which engages into an annular groove on the outer circumference of the piston cover or on the outer circumference of a wearing ring surrounding the piston body.
- a slotted wearing ring which, in the region of its low-pressure side axial end, has a radially inwardly projecting annular projection which engages into an annular groove on the outer circumference of the piston cover or on the outer circumference of a wearing ring surrounding the piston body.
- the piston cover may also carry a wearing ring on its outer circumferential surface in an annular clearance delimited axially toward the high-pressure side by radially projecting projections, the piston cover having passages issuing into the clearance in the circumferential direction between the projections. During the casting operation, melt can enter the annular clearance through these passages and increase the sealing action.
- the end region of the piston rod may be designed in a way known per se as a piston carrier held removably on the piston rod, in order to simplify the production of the piston rod and make it possible to mount different pistons.
- One-piece or even multi-piece pistons for cold chamber casting machines such as are known, for example, from U.S. Pat. No. 5,233,912, WO 03/074211 A or WO 2004/110679 A, have, near their high-pressure side piston end wall, a wearing ring which seals off the piston with respect to the casting cylinder.
- the wearing ring is mostly fixed axially in an annular clearance and is mostly slotted, for example provided with a stepped slot, so that it can spread resiliently open radially in the annular clearance.
- Wearing rings of this type arranged in the region of the cooled piston end wall, seal off the piston sufficiently.
- metal melt can penetrate into the annular clearance and may impede the radial spreadability of the wearing ring there. This leads to increased wear.
- the piston body to carry, in the region of its low-pressure side end, a slotted radially resilient wearing ring, of which the low-pressure side axial end face is exposed over the greater part of its radial thickness with respect to the piston rod.
- a wearing ring arranged on the low-pressure side cleans the casting cylinder of solidified melt residues during the reverse stroke of the piston.
- this wearing ring Since the low-pressure side axial end face of this wearing ring is exposed over the greater part to the casting cylinder surface to be cleaned, with respect to the piston rod, this prevents the surfaces provided for the axial fixing of the wearing ring from being clogged with metal residues removed from the cylinder wall and the wearing ring from becoming jammed or losing its radially resilient properties.
- the casting cylinder has at its low-pressure side end an introduction cone which guides the piston into the casting cylinder.
- the piston With each stroke, the piston is partially drawn out of the casting cylinder, but only to an extent such that its radially springing-open, high-pressure side wearing ring still remains slightly, for example two or three millimeters, in bearing contact with the circular cylindrical surface of the casting cylinder and otherwise overlaps axially with the introduction cone.
- the high-pressure side wearing ring is supplied in the region of the introduction cone with liquid or solid lubricant which lubricates the wearing ring during the working stroke of the piston.
- the low-pressure side wearing ring explained above may be used in pistons with an additional high-pressure side wearing ring, but also in pistons without an additional high-pressure side wearing ring.
- the piston body has at its low-pressure side end, on its outer circumferential surface, an annular clearance open toward the low-pressure side.
- the wearing ring is arranged in its annular clearance and in the region of its high-pressure side axial end has a radially inwardly projecting annular projection which engages into an annular groove on the outer circumference of the piston body.
- Such a wearing ring is exposed completely on its low-pressure side end face.
- the annular projection provided for the axial fixing of said wearing ring is offset with respect to this end face, that is to say does not tend to become jammed.
- the annular projection may alternatively also be provided additionally on the piston body, while the annular groove assigned to it is then provided in the wearing ring.
- a further wearing ring is also provided in the region of the high-pressure side piston end wall.
- This wearing ring is preferably slotted and is designed to be radially resilient and may be arranged in an annular clearance provided on the outer circumferential surface of the piston in the region of the piston end wall and preferably open toward the high-pressure side.
- the high-pressure side and the low-pressure side wearing rings are identical, thus making stockkeeping simpler.
- the low-pressure side wearing ring may likewise have, on its high-pressure side radially outer end region, an introduction cone which makes it easier to introduce the wearing ring into the casting cylinder.
- FIG. 1 shows an exploded illustration of a multi-piece piston according to the invention with an associated piston carrier forming the end region of the piston rod;
- FIG. 2 shows an axial longitudinal section through the piston
- FIG. 3 shows a radial view of a wearing bush of the piston
- FIG. 4 shows a radial view of an abutment element of the piston carrier
- FIG. 5 shows an axial longitudinal half section through a first variant of the piston
- FIG. 6 shows an end view of the piston, as seen in the direction of an arrow VI in FIG. 5 ;
- FIGS. 7 to 10 show axial longitudinal half sections through second to fifth variants of the piston
- FIG. 11 shows a sixth variant of the piston partially in axial longitudinal section.
- FIGS. 1 and 2 show a cap-shaped piston 1 , cooled in a way explained in more detail below, of a cold chamber casting machine for metals, for example aluminum alloys.
- the piston 1 surrounds a piston carrier 3 which itself forms the end region of a piston rod, indicated at 5 , and, for example, is screwed on to this.
- the piston 1 is displaced in a way known per se in a casting cylinder, indicated at 7 , of the cold chamber casting machine.
- the piston 1 is of multi-piece design and comprises a piston cover 9 which, on the high-pressure side of the piston 1 , forms a piston end wall 13 bearing over a large area against an axially normal end face 11 of the piston carrier 3 .
- the piston cover 9 engaging over the end face 11 has adjoining it toward the low-pressure side a piston body 15 which is designed as a bush and which centers radially and is sealed off, fluid-tight, on the high-pressure side at an annular shoulder 17 of the piston cover 9 and, on the low-pressure side, at an annular shoulder 19 of the piston carrier 3 .
- a plurality of screws 23 offset at an angle with respect to one another penetrate through the piston body 15 in axial bores 21 , are screwed into the piston cover 9 from the low-pressure side and combine the piston body 15 with the piston cover 9 to form a structural unit.
- the structural unit of the piston 1 said structural unit consisting of the piston cover 9 and of the piston body 15 , is fastened together axially by means of mutually assigned pairs of bayonet locking members 25 , 27 which are integrally formed, in each case offset in the circumferential direction, on the piston carrier 3 and on the piston cover 9 .
- the bayonet locking members 25 , 27 leave free between them passages 29 and 31 , through which the bayonet locking members 25 , 27 can be inserted axially past one another, before they are locked axially with one another by the piston cover 9 being rotated in relation to the piston carrier 3 .
- a plurality of abutment elements 37 are seated, distributed in the circumferential direction, in respectively assigned countersinks 35 of the piston carrier 3 and are held on the piston carrier 3 by means of radially releasable screws 39 .
- Each of the abutment elements 37 in this case engages into a clearance 41 on the low-pressure side end face 43 of the piston body 15 and positively fixes the piston body 15 and consequently also the piston cover 9 fixedly in terms of rotation on the piston carrier 3 .
- the abutment surface 45 of each abutment element runs so as to be obliquely inclined radially outward with respect to the high-pressure side.
- the oblique abutment surface 45 bears against a codirectionally running abutment countersurface 47 formed by the bottom of the clearance 41 .
- the abutment element 37 is consequently in the form of a wedge which tapers radially inward and which can be drawn out of the clearances 35 , 41 without difficulty in order to release the piston 1 from the piston carrier 3 .
- the piston 1 carries on its outer circumference slotted wearing rings 49 , 51 spreading open radially resiliently.
- the high-pressure side wearing ring 49 is seated in an annular clearance 53 , open toward the high-pressure side, on the outer circumference of the piston cover 9 and has an inner circumferential groove 55 into which a radially outwardly projecting annular collar 57 of the piston cover 9 engages.
- the circumferential groove 55 engages with a radially inwardly projecting annular projection 59 behind the annular collar 57 .
- the low-pressure side wearing ring 51 is in the form of a bush and is received by a clearance 61 , open toward the high-pressure side, of the piston body 15 . For axial fixing, the wearing ring 51 is supported toward the high-pressure side on the piston cover 9 .
- the wearing means 49 , 51 are slotted, their slot edges 63 forming a plurality of steps with circumferentially running step surfaces 65 bearing against one another, as shown in FIG. 3 .
- the high-pressure side wearing ring 49 likewise has a step 65 ′ of the type explained which can be seen in FIG. 1 .
- the cooling fluid for cooling the piston 1 is delivered to the end face 11 via the piston rod 5 and a central duct 67 of the piston carrier 3 .
- Incorporated in the end face 11 are radial ducts 69 in which the cooling fluid is in contact with the piston end wall 13 .
- the cooling fluid flows on the outer circumference of the piston carrier 3 into the region of the low-pressure side end of the piston body 15 , where radial ducts 71 of the piston carrier 3 supply the cooling fluid to a central annular duct 73 of the piston carrier 3 or of the piston rod 5 .
- the piston carrier 3 is provided on its outer circumference with a single-flight or multi-flight helical groove 75 , the turns of which are separated from one another by supporting webs 77 .
- the piston body 15 is supported radially on the supporting webs 77 .
- the grooves 75 form coolant ducts, by which the cooling fluid can come into heat exchange contact with the piston body 15 .
- a multiplicity of mutually parallel circumferential grooves may also be provided, in so far as these are connected to one another by means of axial ducts. It will be appreciated that only axially running grooves may also be provided instead of the grooves 75 running essentially in the circumferential direction.
- FIGS. 5 and 6 show a first variant of a piston 1 a , on which the components and features 3 to 51 and 61 to 77 of the piston 1 of FIGS. 1 to 4 are likewise implemented.
- the high-pressure side, again slotted wearing ring 49 a is seated in a clearance 79 , open toward the low-pressure side, on the circumference of the piston cover 9 a and is fixed axially toward the high-pressure side by means of radial projections 81 .
- a spring ring 83 snapped into an annular clearance of the piston cover 9 a ensures axial fixing toward the low-pressure side.
- the spring ring 83 also assumes the axial fixing of the wearing ring 51 a seated in the clearance 61 a on the outer circumference of the piston body 15 a and designed as a slotted bush.
- passages 85 Provided in the circumferential direction between the radial projections 81 are passages 85 , through which melt can enter the clearance 79 during operation, where it assists the resilient spreading open of the wearing ring 49 a .
- melt can enter the clearance 79 during operation, where it assists the resilient spreading open of the wearing ring 49 a .
- the piston 1 a of FIGS. 5 and 6 comprises, even though this may not be explained in detail, the components 3 to 51 and 61 to 77 of the piston 1 of FIGS. 1 to 4 .
- FIG. 7 shows a piston 1 b which differs from the piston 1 a of FIGS. 5 and 6 in that the high-pressure side wearing ring 49 b is designed as a closed ring and is shrunk with a press fit on to the clearance, open toward the low-pressure side, on the outer circumference of the piston cover 9 b .
- the low-pressure side wearing ring 51 b is fixed axially between the high-pressure side wearing ring 49 b and a low-pressure side shoulder of the clearance 61 b of the piston body 15 b .
- the wearing ring 51 b is designed as a slotted bush in a similar way to the wearing ring of FIG. 3 . Contrary to the piston 1 a of FIGS.
- the radial projection 81 b provided on the piston end face is closed in a circumferential direction. However, its outside diameter is smaller than the outside diameter of the wearing ring 49 b .
- the piston lb comprises the components 3 to 51 and 61 to 77 of the piston 1 of FIGS. 1 to 4 .
- the wearing ring 49 b may also be composed of a plurality of wearing ring elements arranged directly next to one another axially and shrunk on to the piston cover 9 b in the clearance 79 b .
- the multi-piece nature of the wearing ring makes attachment and removal easier.
- the ring elements 49 b ′ and 49 b ′′ may consist of different materials.
- the high-pressure side ring element 49 b ′ may be produced from a more wear-resistant material than the ring element 49 b ′′ and/or the ring element 49 b ′′ may have better sliding properties than the ring element 49 b′′.
- the piston 1 c illustrated in FIG. 8 is a variant of the piston 1 of FIGS. 1 to 4 and differs from this piston essentially only in that the high-pressure side wearing ring 49 c overlaps the low-pressure side wearing ring 51 c axially, the inner annular groove 55 c of the wearing ring 49 c having engaging into it not only the annular projection 57 c of the piston cover 9 c , but also an annular projection 87 provided at the high-pressure side end of the wearing ring 51 c .
- Both wearing rings 49 c and 51 c are again designed as slotted rings, the bush-shaped wearing ring 51 c overlapping axially with the piston cover 9 c and being fixed axially by the projection 57 c .
- the overlapping of the wearing rings 49 c , 51 c increases the sealing action of the piston 1 c .
- the components 3 to 77 of the piston 1 of FIGS. 1 to 4 are also present.
- the piston 1 d illustrated in FIG. 9 is a further variant of the piston 1 of FIGS. 1 to 4 and differs from this piston essentially only in that the piston body 15 d carries no additional wearing ring, but is itself designed as a wearing part.
- the outside diameter of the piston body 15 d is closely adapted to the inside diameter of the casting cylinder.
- the components 3 to 49 and 76 to 77 of the piston 1 of FIGS. 1 to 4 are present.
- the piston cover 9 d extends axially beyond the wearing ring 49 d toward the low-pressure side and on the low-pressure side of the wearing ring 49 d is provided with an annular clearance 89 which directly adjoins the latter and in which metal melt which has gone past the wearing ring 49 d toward the low-pressure side can collect and solidify. The metal residues can thereby be removed from the casting cylinder when the piston 1 d is in its rear end position and consequently essentially outside the casting cylinder.
- FIG. 10 shows a further variant of the piston 1 of FIGS. 1 to 4 .
- the piston le shown in FIG. 10 differs from the piston 1 essentially only in that the piston cover 9 e is itself designed as a wearing part, a high-pressure side wearing ring held on its circumference being dispensed with.
- the outside diameter of the piston cover 9 e is closely adapted to the inside diameter of the casting cylinder.
- the components 3 to 47 , 51 and 61 to 77 of the piston 1 are also implemented on the piston 1 e .
- the piston cover designed as a wearing part may also be used in the piston 1 d of FIG. 9 .
- the piston body 15 d designed as a wearing part, of the piston 1 d from FIG. 9 may also be provided in the variants of FIGS. 5 to 8 , in this case the high-pressure side wearing ring 49 c overlapping axially with the piston body in the piston 1 c of FIG. 8 .
- FIG. 11 shows a further variant of a piston 1 f which differs from the piston 1 d of FIG. 9 essentially only in that a slotted wearing ring 91 is also arranged at the low-pressure side end of the piston body 15 f .
- the wearing ring 91 is identical to the high-pressure side wearing ring 49 f , but is installed in the opposite direction axially. Its stepped slot can be seen at 93 .
- the low-pressure side wearing ring 91 is arranged radially resiliently and consequently expandably in a clearance 95 open toward the low-pressure side of the piston and consequently toward the piston rod 5 f and, at a distance from its axial end face 97 , consequently exposed essentially over the entire height, has an annular groove 99 into which an annular projection 101 projecting radially from the piston body 15 f engages.
- the annular projection 101 fixes the wearing ring 91 radially movably on the piston body 15 f.
- FIG. 11 shows the piston 1 f in its rear end position, drawn out essentially from the casting cylinder 7 f , in which, however, the high-pressure side wearing ring 49 f is still held, compressed, in the circular-cylindrical wall region of the casting cylinder 7 f .
- the wearing ring 49 f in this case otherwise overlaps with an introduction cone 103 at the end of the casting cylinder 7 f , said introduction cone making it easier to introduce the wearing ring 49 f which spreads open outside the casting cylinder 7 f.
- One or more supply ducts 105 via which the wearing ring 49 f can be wetted with a small quantity of lubricant, terminate in the region of the introduction cone 103 .
- the lubricant reduces the friction of the piston against the cylinder wall during the working stroke. It will be appreciated that the lubricant may also be supplied in another way to the wearing ring 49 f overlapping with the introduction cone 103 .
- the lubricant may be a dry, but also a liquid lubricant.
- the wearing ring 91 has a conical chamfer 107 at its radially outer high-pressure side annular edge.
- the wearing ring 91 wipes off melt residues which have possibly remained on the inner wall of the casting cylinder 7 f and thus cleans the casting cylinder 7 f with each stroke. Since the end wall 97 of the wearing ring 91 is exposed and is not overlapped by surfaces for the axial fixing of the wearing ring 91 , the tendency of the wearing ring 91 to become jammed is low.
- the wearing ring 91 may also be provided in the above-explained variants of the multi-piece piston, specifically even when the piston cover is connected in one piece with the piston body and/or the piston has no high-pressure side wearing ring.
- the wearing bushes 51 , 51 a - 51 c and 51 e explained with reference to FIGS. 1 to 8 and 10 may, if appropriate, also be formed by two or more wearing rings arranged axially next to one another, but separated from one another. These wearing rings may themselves be slotted, in particular slotted in a stepped manner, or else be closed annularly. Insofar as the wearing rings are slotted, their radial pressure force can be increased by means of radial springs, such as, for example, helical compression springs, which are seated in blind holes of the piston body.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Pistons, Piston Rings, And Cylinders (AREA)
- Compressor (AREA)
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
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DE102005048717A DE102005048717A1 (de) | 2005-10-12 | 2005-10-12 | Mehrteiliger Kolben für eine Kaltkammer-Giessmaschine |
DE102005048717 | 2005-10-12 | ||
DE102005048717.3 | 2005-10-12 | ||
PCT/EP2006/009831 WO2007042282A2 (de) | 2005-10-12 | 2006-10-11 | Mehrteiliger kolben für eine kaltkammer-giessmaschine |
Publications (2)
Publication Number | Publication Date |
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US20090139683A1 US20090139683A1 (en) | 2009-06-04 |
US8136574B2 true US8136574B2 (en) | 2012-03-20 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US11/992,716 Active 2028-07-21 US8136574B2 (en) | 2005-10-12 | 2006-10-11 | Multi-piece piston for a cold chamber casting machine |
Country Status (13)
Country | Link |
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US (1) | US8136574B2 (de) |
EP (1) | EP1943038B1 (de) |
JP (1) | JP5001284B2 (de) |
KR (1) | KR101334382B1 (de) |
CN (1) | CN101287563B (de) |
AT (1) | ATE454233T1 (de) |
CA (1) | CA2625099C (de) |
DE (2) | DE102005048717A1 (de) |
DK (1) | DK1943038T3 (de) |
ES (1) | ES2339054T3 (de) |
HK (1) | HK1125892A1 (de) |
PL (1) | PL1943038T3 (de) |
WO (1) | WO2007042282A2 (de) |
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WO2015054776A1 (en) | 2013-10-18 | 2015-04-23 | Exco Technologies Limited | Wear ring for die-casting piston, die-casting piston incorporating same, and method of forming same |
US20160038998A1 (en) * | 2013-04-04 | 2016-02-11 | Gani MURSELAJ | Piston for metal die casting |
US20170066047A1 (en) * | 2014-02-21 | 2017-03-09 | Alrotec Tecnology, S.L.U. | Piston for cold-chamber injection machines |
US10603715B2 (en) | 2016-12-30 | 2020-03-31 | Exco Technologies Limited | Die-casting piston, and die-casting apparatus incorporating same |
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US20090160106A1 (en) * | 2004-10-12 | 2009-06-25 | Efficient Manufacturing System Integration | Apparatus and method for simultaneous usage of multiple die casting tools |
WO2009146568A1 (de) * | 2008-06-05 | 2009-12-10 | Mueller Andre | Giesskolben zum einsetzen in einer giesskammer |
IT1393330B1 (it) | 2009-01-21 | 2012-04-20 | Brondolin S P A | Pistoni per pressofusione |
IT1393329B1 (it) * | 2009-01-21 | 2012-04-20 | Brondolin S P A | Pistone e anello di tenuta per pressofusione |
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CN104493126B (zh) * | 2014-12-09 | 2016-04-06 | 高要市力源压铸有限公司 | 一种压铸机压射冲头的润滑冷却方法及装置 |
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- 2006-10-11 CN CN2006800379755A patent/CN101287563B/zh active Active
- 2006-10-11 CA CA2625099A patent/CA2625099C/en active Active
- 2006-10-11 JP JP2008534929A patent/JP5001284B2/ja active Active
- 2006-10-11 DK DK06806194.4T patent/DK1943038T3/da active
- 2006-10-11 PL PL06806194T patent/PL1943038T3/pl unknown
- 2006-10-11 EP EP06806194A patent/EP1943038B1/de active Active
- 2006-10-11 WO PCT/EP2006/009831 patent/WO2007042282A2/de active Application Filing
- 2006-10-11 AT AT06806194T patent/ATE454233T1/de active
- 2006-10-11 US US11/992,716 patent/US8136574B2/en active Active
- 2006-10-11 KR KR1020087011262A patent/KR101334382B1/ko active IP Right Grant
- 2006-10-11 ES ES06806194T patent/ES2339054T3/es active Active
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2009
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Cited By (7)
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US20160038998A1 (en) * | 2013-04-04 | 2016-02-11 | Gani MURSELAJ | Piston for metal die casting |
US9463505B2 (en) * | 2013-04-04 | 2016-10-11 | Gani MURSELAJ | Piston for metal die casting |
EP2796226A1 (de) | 2013-04-24 | 2014-10-29 | HTS IC d.o.o. | Kolben mit optimaler Kühlwirkung für Kaltkammerdruckgusssysteme |
WO2015054776A1 (en) | 2013-10-18 | 2015-04-23 | Exco Technologies Limited | Wear ring for die-casting piston, die-casting piston incorporating same, and method of forming same |
US20170066047A1 (en) * | 2014-02-21 | 2017-03-09 | Alrotec Tecnology, S.L.U. | Piston for cold-chamber injection machines |
US9962762B2 (en) * | 2014-02-21 | 2018-05-08 | Alrotec Technology, S.L.U. | Piston for cold-chamber injection machines |
US10603715B2 (en) | 2016-12-30 | 2020-03-31 | Exco Technologies Limited | Die-casting piston, and die-casting apparatus incorporating same |
Also Published As
Publication number | Publication date |
---|---|
ES2339054T3 (es) | 2010-05-14 |
HK1125892A1 (en) | 2009-08-21 |
WO2007042282A3 (de) | 2007-08-02 |
KR101334382B1 (ko) | 2013-11-29 |
JP2009511275A (ja) | 2009-03-19 |
EP1943038B1 (de) | 2010-01-06 |
ATE454233T1 (de) | 2010-01-15 |
CA2625099A1 (en) | 2007-04-19 |
US20090139683A1 (en) | 2009-06-04 |
DE502006005883D1 (de) | 2010-02-25 |
DK1943038T3 (da) | 2010-05-10 |
KR20080059642A (ko) | 2008-06-30 |
EP1943038A2 (de) | 2008-07-16 |
WO2007042282A2 (de) | 2007-04-19 |
CN101287563B (zh) | 2011-09-07 |
CA2625099C (en) | 2015-02-17 |
CN101287563A (zh) | 2008-10-15 |
PL1943038T3 (pl) | 2010-07-30 |
JP5001284B2 (ja) | 2012-08-15 |
DE102005048717A1 (de) | 2007-04-19 |
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